JP2014065481A - 予荷重を減少させたロンチロック組立体、およびそれを含む宇宙船制振システム - Google Patents
予荷重を減少させたロンチロック組立体、およびそれを含む宇宙船制振システム Download PDFInfo
- Publication number
- JP2014065481A JP2014065481A JP2013150439A JP2013150439A JP2014065481A JP 2014065481 A JP2014065481 A JP 2014065481A JP 2013150439 A JP2013150439 A JP 2013150439A JP 2013150439 A JP2013150439 A JP 2013150439A JP 2014065481 A JP2014065481 A JP 2014065481A
- Authority
- JP
- Japan
- Prior art keywords
- tooth ring
- assembly
- mounting portion
- transverse tooth
- retracting
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 230000000712 assembly Effects 0.000 title claims abstract description 29
- 238000000429 assembly Methods 0.000 title claims abstract description 29
- 230000036316 preload Effects 0.000 title abstract description 20
- 238000002955 isolation Methods 0.000 title description 2
- 230000033001 locomotion Effects 0.000 claims description 11
- 230000004323 axial length Effects 0.000 claims description 4
- 238000013016 damping Methods 0.000 description 48
- 238000006243 chemical reaction Methods 0.000 description 5
- 230000001629 suppression Effects 0.000 description 5
- 230000005540 biological transmission Effects 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 229910001285 shape-memory alloy Inorganic materials 0.000 description 4
- 230000008602 contraction Effects 0.000 description 3
- 230000003287 optical effect Effects 0.000 description 3
- 229910045601 alloy Inorganic materials 0.000 description 2
- 239000000956 alloy Substances 0.000 description 2
- 230000003321 amplification Effects 0.000 description 2
- 238000003491 array Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000005284 excitation Effects 0.000 description 2
- 238000003199 nucleic acid amplification method Methods 0.000 description 2
- 229910000851 Alloy steel Inorganic materials 0.000 description 1
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 239000004606 Fillers/Extenders Substances 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000006870 function Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- 229910001000 nickel titanium Inorganic materials 0.000 description 1
- HLXZNVUGXRDIFK-UHFFFAOYSA-N nickel titanium Chemical compound [Ti].[Ti].[Ti].[Ti].[Ti].[Ti].[Ti].[Ti].[Ti].[Ti].[Ti].[Ni].[Ni].[Ni].[Ni].[Ni].[Ni].[Ni].[Ni].[Ni].[Ni].[Ni].[Ni].[Ni].[Ni] HLXZNVUGXRDIFK-UHFFFAOYSA-N 0.000 description 1
- 238000012827 research and development Methods 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
- B64G1/641—Interstage or payload connectors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/228—Damping of high-frequency vibration effects on spacecraft elements, e.g. by using acoustic vibration dampers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
- B64G1/283—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using reaction wheels
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
- B64G1/285—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using momentum wheels
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
- B64G1/286—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using control momentum gyroscopes (CMGs)
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Clamps And Clips (AREA)
Abstract
【解決手段】ロンチロック組立体34は、第1の取付け部36および第2の取付け部38と、解除可能な締め付けデバイスと、一対の後退組立体とを備える。各後退組立体が、相互作用する歯付き面を有する一対の歯付き部材を備える。解除可能な締め付けデバイスは、第1の取付け部および第2の取付け部を締め付け係合で通常保持する。解除可能な締め付けデバイスが作動されると第1の取付け部および第2の取付け部が締め付け係合から解除され、各後退組立体の一方の歯付き部材が、他方の後退組立体の他方の1つの歯付き部材に対して反対方向に移動して、第1の取付け部のそれぞれの側に軸方向間隙を画定する。
【選択図】図1
Description
本発明は、NASAによって授与されたNNG09HR00Cの下で政府の支援によってなされた。政府は、本発明における一定の権利を有する。
22 ペイロード
24 宇宙母船、宇宙船
26 複数の1自由度または軸方向減衰式の振動絶縁装置、振動絶縁装置、制振装置
28 ペイロード支持構造
30 宇宙船マウント用インタフェース
32 複数の取り付け用固定金具
34 ロンチロック組立体
36 第1の取付け部
38 第2の取付け部
42 ロンチロック組立体
44 上側取付け部、取付け部、第1の取付け部
45 隆起した環状リム、環状リム
46 下側取付け部、取付け部
48 周方向フランジ、取付けフランジ
50 留め具の開口
52 ほぼ円筒形の内側ボアまたは空洞、内側空洞、空洞、内部空洞
54 ほぼ円筒形の内側ボアまたは空洞、内側空洞、空洞
56 下側末端壁、末端壁
58 接触面、下側接触面、第1の接触面
59 斜めに対向した面取りした接触面、第1の面取りした接触面、接触面
60 接触面、第2の接触面
61 斜めに対向した面取りした接触面、第2の面取りした接触面、接触面
62 内側環状突起部
64 解除可能な締め付けデバイス
66 後退組立体、第1の上側後退組立体
68 摺動締め付け部材、締め付け部材、スライド移動締め付け部材
70 軸方向に伸縮可能なボルト、ボルト
72 ボルト伸縮アクチュエータ
74 細長い管状の本体、管状の本体
76 径方向に拡大した円筒形のヘッドまたはキャップ、円筒形のキャップ、キャップ径方向に拡大したキャップ
78 鍵
80 径方向に拡大したヘッド、ボルトヘッド
82 ナット
84 丸く囲まれた領域、第1の環状の締め付け面、環状の締め付け面
85 丸く囲まれた領域
88 SMAコア、コア
90 回路ヒータ、ヒータ
92 断熱ワッシャ、絶縁ワッシャ
94 波形ばね
96 窓
98 第1の横歯リング、横歯リング
100 第2の横歯リング
102 環状体
104 複数のブロック状の歯
106 環状体
108 歯
110 引張ばね
112 鉤付きの軸方向突出部
114 取付けフランジ
116小さい軸方向のステップ
124 第1の軸方向間隙
166 後退組立体、第2の下側後退組立体
198 横歯リング、第2の一対の横歯リング、第1の横歯リング
200 横歯リング、第2の一対の横歯リング、第2の横歯リング
204 ブロック状の歯
206 環状体
208 複数のブロック状の歯、各歯
210 引張ばね
216小さい軸方向のステップ
Claims (3)
- 第1の取付け部および第2の取付け部と、
前記第1の取付け部および前記第2の取付け部を締め付け係合で通常保持し、作動されると前記第1の取付け部および前記第2の取付け部を締め付け係合から解除する解除可能な締め付けデバイスと、
各後退組立体が第1の横歯リングおよび第2の横歯リングを備える一対の後退組立体であって、各後退組立体の前記第2の横歯リングが、他方の後退組立体の前記第2の横歯リングに対して反対方向に移動するようになされて、前記解除可能な締め付けデバイスが作動されるときに前記第1の取付け部のそれぞれの側に軸方向間隙を生じさせる一対の後退組立体と
を備えるロンチロック組立体。 - 前記一対の後退組立体が、第1の後退組立体および第2の後退組立体を備え、前記第1の取付け部が、
内部に前記解除可能な締め付けデバイスおよび前記一対の後退組立体が配設される中央開口を有するほぼ管状の本体と、
前記ほぼ管状の本体から径方向内側に延びる内側環状突出部と
を備え、前記第1の取付け部および前記第2の取付け部が締め付け係合にあるときに、前記内側環状突出部が、前記第1の後退組立体の前記第2の横歯リングと前記第2の後退組立体の前記第2の横歯リングとの間に捕らえられ、前記第2の後退組立体の前記第2の横歯リングが、一対の斜めに対向した面取りした接触面を含み、前記第1の取付け部および前記第2の取付け部が締め付け係合にあるときに、前記一対の斜めに対向した面取りした接触面の第1の面取りした接触面が、前記第1の取付け部の前記内側環状突出部に係合可能であり、前記一対の第2の面取りした接触面が、前記第2の後退組立体の前記第1の横歯リングに係合可能である、
請求項1に記載のロンチロック組立体。 - 各後退組立体の前記第2の横歯リングは、
(i) 前記第2の横歯リングの歯が、同じ後退組立体の前記第1の横歯リングの歯に先端と先端で係合する軸方向拡大位置に通常はあり、
(ii) 前記第2の横歯リングの前記歯が、前記同じ後退組立体の前記第1の横歯リングの前記歯に先端と根本で係合する軸方向に崩れた位置に向かって付勢されて、それぞれの各後退組立体の軸方向長さを減少させ、
作動されると、前記解除可能な締め付けデバイスが、前記第1の取付け部および前記第2の取付け部を締め付け係合から解除して、各後退組立体の前記第2の横歯リングが前記軸方向に崩れた位置に移動することを可能にし、前記第1の取付け部のそれぞれの側に前記軸方向間隙を形成する、請求項1に記載のロンチロック組立体。
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/626,843 US9475594B2 (en) | 2012-09-25 | 2012-09-25 | Launch lock assemblies with reduced preload and spacecraft isolation systems including the same |
US13/626,843 | 2012-09-25 |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2014065481A true JP2014065481A (ja) | 2014-04-17 |
JP6199103B2 JP6199103B2 (ja) | 2017-09-20 |
Family
ID=48793930
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2013150439A Active JP6199103B2 (ja) | 2012-09-25 | 2013-07-19 | 予荷重を減少させたロンチロック組立体、およびそれを含む宇宙船制振システム |
Country Status (3)
Country | Link |
---|---|
US (1) | US9475594B2 (ja) |
EP (1) | EP2711300B1 (ja) |
JP (1) | JP6199103B2 (ja) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11981458B2 (en) | 2019-11-07 | 2024-05-14 | Exolaunch Gmbh | Separation system for a satellite |
Families Citing this family (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2013052626A1 (en) * | 2011-10-05 | 2013-04-11 | The Unversity Of Akron | Reduced shock breakaway set screw for use with a surgical construct |
JP6581601B2 (ja) * | 2014-05-19 | 2019-09-25 | マクドナルド デットワイラー アンド アソシエイツ インコーポレーテッド | ペイロード射出システム |
US9739336B2 (en) * | 2014-08-13 | 2017-08-22 | Northrop Grumman Systems Corporation | Magnetically damped isolator and pointing mount |
JP6299558B2 (ja) * | 2014-10-28 | 2018-03-28 | アイシン精機株式会社 | 車体補強装置 |
EP3029777B1 (en) * | 2014-12-02 | 2018-09-05 | ABB Schweiz AG | Electrical connection for medium and high voltage switchgears |
FR3041327B1 (fr) * | 2015-09-18 | 2019-05-31 | Thales | Actionneur gyroscopique a double guidage cardan, element de suspension et element de butee |
US9796488B2 (en) * | 2015-10-02 | 2017-10-24 | The Boeing Company | Dual port payload attach ring compatible satellite |
US9828117B2 (en) * | 2016-02-04 | 2017-11-28 | United Launch Alliance, L.L.C. | Tensioning apparatus and system for clamping joints |
US10451139B2 (en) | 2017-11-30 | 2019-10-22 | Honeywell International Inc. | Damping coefficient-regulating inductive heating systems and isolator assemblies including the same |
US11021271B2 (en) | 2018-05-10 | 2021-06-01 | SpinLaunch Inc. | Ruggedized reaction wheel for use on kinetically launched satellites |
CN109264035B (zh) * | 2018-10-11 | 2021-03-16 | 北京航空航天大学 | 一种航天器“连杆——卡爪”式对接锁紧装置 |
CN110329552A (zh) * | 2019-08-08 | 2019-10-15 | 北京微分航宇科技有限公司 | 一种多点压紧同步解锁的星箭适配器 |
US11794927B2 (en) | 2019-08-28 | 2023-10-24 | The Boeing Company | Additively manufactured spacecraft panel |
AU2019473170A1 (en) * | 2019-11-07 | 2022-03-03 | Exolaunch Gmbh | Separation system for a satellite |
US11483942B2 (en) | 2019-12-18 | 2022-10-25 | SpinLaunch Inc. | Ruggedized avionics for use on kinetically launched vehicles |
US11827389B2 (en) | 2020-05-18 | 2023-11-28 | The Boeing Company | Additively manufactured satellite |
US11802606B2 (en) * | 2020-05-18 | 2023-10-31 | The Boeing Company | Planate dynamic isolator |
CN112777004B (zh) * | 2020-10-29 | 2022-09-27 | 北京卫星制造厂有限公司 | 一种用于线式低冲击分离装置的大减力比低冲击释放机构 |
CA3140350A1 (en) | 2020-12-17 | 2022-06-17 | The Boeing Company | Satellite thermal enclosure |
CN114516430B (zh) * | 2022-01-25 | 2023-07-25 | 上海卫星工程研究所 | 适用于维修升级卫星的同构式在轨对接装置 |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5340164A (en) * | 1976-09-25 | 1978-04-12 | Mitsubishi Heavy Ind Ltd | Vibration-proof elastic-support fixing system |
US5160233A (en) * | 1992-05-13 | 1992-11-03 | The United State Of America As Representd By The Administrator Of The National Aeronautics And Space Administration | Fastening apparatus having shape memory alloy actuator |
US6508437B1 (en) * | 2002-01-15 | 2003-01-21 | Honeywell International Inc. | Launch lock for spacecraft payloads |
Family Cites Families (67)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US962246A (en) | 1905-03-07 | 1910-06-21 | New Departure Mfg Co | Pneumatic spring. |
US2000172A (en) | 1933-10-23 | 1935-05-07 | American Seating Co | Hinge |
US2766079A (en) | 1952-05-09 | 1956-10-09 | William H Browne | Rod end bearing |
US3085773A (en) | 1960-02-01 | 1963-04-16 | North American Aviation Inc | Adjustable engine mount |
US3182329A (en) | 1963-06-13 | 1965-05-04 | Illinois Tool Works | Antenna mounting clip |
DE1196494B (de) | 1963-08-24 | 1965-07-08 | Agfa Ag | Fotografischer Zweisektorenverschluss |
US3288421A (en) | 1965-03-29 | 1966-11-29 | Everett R Peterson | Movable and rotatable top |
DE1255518B (de) | 1965-12-28 | 1967-11-30 | Rheinstahl Henschel Ag | Gelenk fuer Lenk- bzw. Spurstangen von Fahrzeugen mit mehreren Stangen |
US3405593A (en) | 1966-04-18 | 1968-10-15 | Aerospace Systems Company | Separation device |
US3512162A (en) | 1967-10-02 | 1970-05-12 | Gen Electric | Combination vhf antenna mounting clip and signal transfer |
US3525448A (en) | 1968-05-17 | 1970-08-25 | Clark Equipment Co | Pivotal joint with ball-bushing and countersunk pin |
US3635427A (en) | 1969-05-06 | 1972-01-18 | Textron Inc | Aircraft vibration compensation system |
US3577659A (en) | 1969-08-06 | 1971-05-04 | Singer General Precision | Motion simulator actuator joint |
US3699580A (en) | 1971-01-18 | 1972-10-17 | Gen Electric | Antenna mounting clip |
US3794277A (en) | 1972-08-14 | 1974-02-26 | A Smedley | Earthquake resistant support |
US4054186A (en) | 1975-04-10 | 1977-10-18 | Barry Wright Corporation | Snubber apparatus |
US3983965A (en) | 1975-07-07 | 1976-10-05 | Pacific Scientific Company | Adjustable locking strut |
US3981467A (en) * | 1975-10-17 | 1976-09-21 | The United States Of America As Represented By The Secretary Of The Air Force | Launch lock device |
US4185720A (en) | 1976-06-11 | 1980-01-29 | Pacific Scientific Company | Adjustable locking strut |
DE2802791A1 (de) | 1978-01-23 | 1979-07-26 | Niedecker Herbert | Vorrichtung zum bestimmen und spannen von werkstuecken |
US4243192A (en) | 1978-12-04 | 1981-01-06 | Mcdonnell Douglas Corporation | Ball pivot thrust bearing flex joint |
US4360284A (en) | 1980-10-08 | 1982-11-23 | General Motors Corporation | Ball-joint assembly |
US4515336A (en) | 1983-04-14 | 1985-05-07 | Opcon, Inc. | Ball and socket mount for optical sensing system source and/or detector devices |
FR2648199B1 (fr) | 1989-06-09 | 1991-09-27 | Aerospatiale | Dispositif de liaison temporaire, notamment pour appendice de satellite artificiel, et procede de liberation d'une telle liaison |
US5028180A (en) | 1989-09-01 | 1991-07-02 | Sheldon Paul C | Six-axis machine tool |
US5069571A (en) | 1990-02-07 | 1991-12-03 | Seals-It, Inc. | Rod end assembly |
US5209596A (en) | 1990-02-07 | 1993-05-11 | Matczak Stanley E | Seal component and rod end assembly utilizing same |
US5040748A (en) | 1990-02-20 | 1991-08-20 | General Dynamics Corporation/Space Systems Division | Payload adapter ring |
US5199690A (en) | 1990-07-26 | 1993-04-06 | M/Rad Corporation | Active vibration isolation system |
US5190423A (en) | 1991-02-15 | 1993-03-02 | Ewing Paul E | Locking fastener |
GB9114124D0 (en) | 1991-06-29 | 1991-08-14 | Rediffusion Simulation Ltd | Actuator assembly |
US5620154A (en) | 1995-05-03 | 1997-04-15 | The Boeing Company | Three link failsafe engine mount |
US5722709A (en) | 1996-10-30 | 1998-03-03 | Hughes Electronics | Separation device using a shape memory alloy retainer |
US6126115A (en) | 1997-01-21 | 2000-10-03 | Lockheed Martin Corporation | Apparatus for retaining and releasing a payload |
US6350074B1 (en) | 1998-06-08 | 2002-02-26 | Northrop Grumman Corporation | Spherical clevis assembly |
FR2787152B1 (fr) | 1998-12-11 | 2001-02-16 | Eurocopter France | Dispositif a doigt pour le blocage d'une piece par rapport a une autre |
US6135401A (en) | 1998-12-23 | 2000-10-24 | Chen; Shi-Jia | Tool for supporting objects |
US6467987B1 (en) | 1999-03-29 | 2002-10-22 | Honeywell International Inc. | Resettable non-explosive actuator |
US6330995B1 (en) | 2000-02-29 | 2001-12-18 | General Electric Company | Aircraft engine mount |
US6352397B1 (en) | 2000-05-31 | 2002-03-05 | Hi-Shear Technology Corporation | Reduced shock separation fastener |
US6769830B1 (en) | 2000-07-05 | 2004-08-03 | Lockheed Martin Corporation | Connector assembly |
ES2188331B1 (es) | 2000-09-20 | 2004-06-16 | Sener, Ingenieria Y Sistemas, S.A. | Mecanismo de amarre y liberacion de equipos con actuacion remota. |
FR2825766B1 (fr) | 2001-06-08 | 2003-10-10 | Lacroix Soc E | Mecanisme a liberation controlee par un effet thermique |
US6669393B2 (en) | 2001-10-10 | 2003-12-30 | General Electric Co. | Connector assembly for gas turbine engines |
US7001127B2 (en) * | 2003-10-20 | 2006-02-21 | Hi-Shear Technology | Non-pyrolytically actuated reduced-shock separation fastener |
US6843449B1 (en) | 2004-02-09 | 2005-01-18 | General Electric Company | Fail-safe aircraft engine mounting system |
FR2867155B1 (fr) | 2004-03-08 | 2007-06-29 | Snecma Moteurs | Suspension d'un moteur a la structure d'un avion |
DE102005010708B4 (de) | 2005-03-09 | 2007-03-15 | Häfner & Krullmann Gmbh | Verbindungssystem |
US7878448B2 (en) | 2005-04-04 | 2011-02-01 | Lord Corporation | Aircraft auxiliary power unit suspension system for isolating an aircraft auxiliary power unit |
FR2907177B1 (fr) | 2006-10-13 | 2009-12-04 | Snecma | Assemblage d'un dispositif rotulant sur une chape de renvoi d'angle, systeme de commande d'un redresseur a calage variable le comportant, et moteur d'aeronef en etant muni |
US7953523B2 (en) | 2007-03-16 | 2011-05-31 | Honeywell International Inc. | Active control of soft hybrid isolation systems |
US8973724B2 (en) | 2007-07-17 | 2015-03-10 | Honeywell International Inc. | Vibration isolators and isolation systems |
CN101376061B (zh) | 2007-08-31 | 2011-06-08 | 鸿富锦精密工业(深圳)有限公司 | 关节 |
US8371534B1 (en) | 2007-09-14 | 2013-02-12 | Lockheed Martin Corporation | System for isolating vibration among a plurality of instruments |
US8002251B2 (en) | 2007-11-14 | 2011-08-23 | Honeywell International Inc. | Vibration reduction system employing active bearing mounts |
US8444121B2 (en) | 2008-03-31 | 2013-05-21 | Honeywell International Inc. | Systems for damping vibrations from a payload |
US7677522B2 (en) | 2008-05-07 | 2010-03-16 | Bakos Stephen M | Support bracket for a column |
FR2932164B1 (fr) * | 2008-06-06 | 2010-08-20 | Thales Sa | Dispositif de maintien d'au moins un objet mobile, reutilisable, securise autonome et sans chocs, pour engins spatiaux |
US7967282B2 (en) | 2008-10-23 | 2011-06-28 | Honeywell International Inc. | Vibration isolators |
US8327985B2 (en) * | 2009-06-22 | 2012-12-11 | Honeywell International Inc. | Two stage vibration isolator |
CN101994896A (zh) | 2009-08-17 | 2011-03-30 | 鸿富锦精密工业(深圳)有限公司 | 连接装置 |
DE102010029651A1 (de) | 2010-06-02 | 2011-12-08 | Carl Zeiss Smt Gmbh | Verfahren zum Betrieb einer Projektionsbelichtungsanlage für die Mikrolithographie mit Korrektur von durch rigorose Effekte der Maske induzierten Abbildungsfehlern |
US8550408B2 (en) | 2010-07-16 | 2013-10-08 | The Boeing Company | Dual evolved expendable launch vehicle (EELV) secondary payload adaptor (ESPA) port small satellite design |
KR101403026B1 (ko) | 2010-10-29 | 2014-06-03 | 한국전자통신연구원 | 우주용 무충격 분리장치 |
US8708322B2 (en) | 2010-11-05 | 2014-04-29 | Honeywell International Inc. | Payload launch lock mechanism |
US8956068B2 (en) | 2011-01-05 | 2015-02-17 | King Fahd University Of Petroleum And Minerals | Kinematic platform |
US8678323B2 (en) | 2012-02-28 | 2014-03-25 | Honeywell International Inc. | Launch lock assemblies including axial gap amplification devices and spacecraft isolation systems including the same |
-
2012
- 2012-09-25 US US13/626,843 patent/US9475594B2/en active Active
-
2013
- 2013-07-12 EP EP13176380.7A patent/EP2711300B1/en active Active
- 2013-07-19 JP JP2013150439A patent/JP6199103B2/ja active Active
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5340164A (en) * | 1976-09-25 | 1978-04-12 | Mitsubishi Heavy Ind Ltd | Vibration-proof elastic-support fixing system |
US5160233A (en) * | 1992-05-13 | 1992-11-03 | The United State Of America As Representd By The Administrator Of The National Aeronautics And Space Administration | Fastening apparatus having shape memory alloy actuator |
US6508437B1 (en) * | 2002-01-15 | 2003-01-21 | Honeywell International Inc. | Launch lock for spacecraft payloads |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11981458B2 (en) | 2019-11-07 | 2024-05-14 | Exolaunch Gmbh | Separation system for a satellite |
Also Published As
Publication number | Publication date |
---|---|
JP6199103B2 (ja) | 2017-09-20 |
EP2711300A2 (en) | 2014-03-26 |
US9475594B2 (en) | 2016-10-25 |
EP2711300B1 (en) | 2018-07-04 |
US20140084113A1 (en) | 2014-03-27 |
EP2711300A3 (en) | 2017-10-11 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP6199103B2 (ja) | 予荷重を減少させたロンチロック組立体、およびそれを含む宇宙船制振システム | |
JP6045331B2 (ja) | 軸方向の空隙増幅装置を含む発射ロック組立体およびこの組立体を含む宇宙機分離システム | |
EP1606164B1 (en) | Remotely releasable support strut | |
JP2009511319A (ja) | 打ち上げロケットと衛星を連結および分離する装置 | |
JPH10159898A (ja) | 多次元振動外乱の遮断装置 | |
JP2011102118A (ja) | 宇宙用の付属品を保持し、衝撃を伴わずに解放できるようにする能動的なタイロッドシステム | |
US9416842B2 (en) | Isolators having damper-external thermal compensators and spacecraft isolation systems employing the same | |
JP5981559B2 (ja) | 振動絶縁システム及び方法 | |
US10723488B2 (en) | Device for retaining and releasing appendages | |
US7503431B2 (en) | Mechanical rotational drive | |
US10240885B2 (en) | Shock absorbing disruptor mounting system | |
KR20120072475A (ko) | 형상기억합금 실린더와 형상기억합금 와이어를 이용한 저충격 비폭발식 분리장치, 그 분리장치의 설치방법, 분리시스템, 준비방법, 분리방법 및 재조립방법 | |
JP2018529569A (ja) | 2つの部品間の制御された分離を行うための装置、およびこのような装置の使用 | |
JP5318483B2 (ja) | 制震装置 | |
JP2015102244A (ja) | 入れ子式フレキシャデバイスを有するアイソレータおよびその製造のための方法 | |
Barber et al. | Launch lock assemblies with reduced preload and spacecraft isolation systems including the same | |
EP3350075B1 (en) | Aircraft support structures, systems, and methods | |
KR102325955B1 (ko) | 진동절연 장치 | |
JP6569073B1 (ja) | 制振装置、及びそれを備えた建築材 | |
JP6415138B2 (ja) | 張力材用制振装置 | |
JP2008127859A (ja) | 制震構造及び制震パネル | |
JP6878757B1 (ja) | 制振装置、及びそれを備えた建築材 | |
JP2021113610A (ja) | 固定隔離器及びシステムを隔離する方法 | |
KR20190105407A (ko) | 가스터빈 엔진의 지지 장치 | |
JP2018108804A (ja) | 3つのバネを具備するラムエアタービンアクチュエータ |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
A621 | Written request for application examination |
Free format text: JAPANESE INTERMEDIATE CODE: A621 Effective date: 20160719 |
|
A977 | Report on retrieval |
Free format text: JAPANESE INTERMEDIATE CODE: A971007 Effective date: 20170413 |
|
A131 | Notification of reasons for refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A131 Effective date: 20170417 |
|
A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20170710 |
|
TRDD | Decision of grant or rejection written | ||
A01 | Written decision to grant a patent or to grant a registration (utility model) |
Free format text: JAPANESE INTERMEDIATE CODE: A01 Effective date: 20170725 |
|
A61 | First payment of annual fees (during grant procedure) |
Free format text: JAPANESE INTERMEDIATE CODE: A61 Effective date: 20170823 |
|
R150 | Certificate of patent or registration of utility model |
Ref document number: 6199103 Country of ref document: JP Free format text: JAPANESE INTERMEDIATE CODE: R150 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |